US4209570A - Homogeneous brazing foils of copper based metallic glasses - Google Patents
Homogeneous brazing foils of copper based metallic glasses Download PDFInfo
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- US4209570A US4209570A US05/947,329 US94732978A US4209570A US 4209570 A US4209570 A US 4209570A US 94732978 A US94732978 A US 94732978A US 4209570 A US4209570 A US 4209570A
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- brazing
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- foil
- copper
- metal
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- 238000005219 brazing Methods 0.000 title claims abstract description 58
- 239000011888 foil Substances 0.000 title claims abstract description 46
- 239000010949 copper Substances 0.000 title claims abstract description 38
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 title claims abstract description 30
- 229910052802 copper Inorganic materials 0.000 title claims abstract description 30
- 239000005300 metallic glass Substances 0.000 title abstract description 15
- 239000000203 mixture Substances 0.000 claims abstract description 31
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 27
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 12
- 239000011574 phosphorus Substances 0.000 claims abstract description 12
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 10
- 239000012535 impurity Substances 0.000 claims abstract description 9
- 229910045601 alloy Inorganic materials 0.000 abstract description 33
- 239000000956 alloy Substances 0.000 abstract description 33
- 229910052751 metal Inorganic materials 0.000 abstract description 31
- 239000002184 metal Substances 0.000 abstract description 31
- 239000000945 filler Substances 0.000 abstract description 18
- 229910001092 metal group alloy Inorganic materials 0.000 abstract description 12
- 229910000881 Cu alloy Inorganic materials 0.000 abstract description 5
- 125000004429 atom Chemical group 0.000 description 19
- 239000000463 material Substances 0.000 description 17
- 238000000034 method Methods 0.000 description 17
- 230000008569 process Effects 0.000 description 13
- 239000000843 powder Substances 0.000 description 10
- 230000008018 melting Effects 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 238000004455 differential thermal analysis Methods 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 7
- 239000000155 melt Substances 0.000 description 6
- 239000011230 binding agent Substances 0.000 description 5
- 229910052752 metalloid Inorganic materials 0.000 description 5
- 238000010791 quenching Methods 0.000 description 5
- 238000001816 cooling Methods 0.000 description 4
- 238000002425 crystallisation Methods 0.000 description 4
- 230000008025 crystallization Effects 0.000 description 4
- 238000005304 joining Methods 0.000 description 4
- 230000000171 quenching effect Effects 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- 229910018104 Ni-P Inorganic materials 0.000 description 3
- 229910018536 Ni—P Inorganic materials 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 229910052723 transition metal Inorganic materials 0.000 description 3
- 150000003624 transition metals Chemical class 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000010953 base metal Substances 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910017758 Cu-Si Inorganic materials 0.000 description 1
- 229910017931 Cu—Si Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 125000005843 halogen group Chemical group 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 229910052809 inorganic oxide Inorganic materials 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000075 oxide glass Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 238000010561 standard procedure Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 238000007740 vapor deposition Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C45/00—Amorphous alloys
- C22C45/001—Amorphous alloys with Cu as the major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
- B23K35/0233—Sheets, foils
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/302—Cu as the principal constituent
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12431—Foil or filament smaller than 6 mils
Definitions
- This invention relates to copper based metal alloys and more particularly to a homogeneous, ductile brazing material useful for brazing metal articles such as those composed of copper and copper alloys.
- Brazing is a process for joining metal parts, often of dissimilar composition, to each other.
- a filler metal that has a melting point lower than that of the metal parts to be joined together is interposed between the metal parts to form an assembly.
- the assembly is then heated to a temperature sufficient to melt the filler metal. Upon cooling, a strong, corrosion resistant, leaktight joint is formed.
- brazing alloys suitable for use with copper and copper alloys designated AWS BCuP are well known compositions. These alloys contain a substantial amount (about 5 to 7.5 weight percent) of the metalloid element phosphorus. Consequently, such alloys are very brittle and are available only as powder or cast rod. Powders are generally unsuitable for many brazing operations, such as dip brazing, and do not easily permit brazing of complex shapes. Although some powders are available as pastes employing organic binders, the binders form objectionable voids and residues during brazing. Rods must be melted outside the joint and, when molten, are fed into the joint by capillary action.
- brazing alloys are available in foil form. However, such materials are either fabricated only through a costly sequence of rolling and careful heat-treating steps or are prepared by powder metallurgical techniques. Rolled foil is not sufficiently ductile to permit stamping of complex shapes therefrom. Powder metallurgical foil is not homogeneous and employes binders, which form objectionable voids and residues during brazing.
- Ductile glassy metal alloys have been disclosed in U.S. Pat. No. 3,856,513, issued Dec. 24, 1974 to H. S. Chen et al. These alloys include compositions having the formula T i X j , where T is at least one transition metal and X is an element selected from the group consisting of phosphorus, boron, carbon, aluminum, silicon, tin, germanium, indium, beryllium and antimony, "i” ranges from about 70 to about 87 atom percent and "j" ranges from about 13 to 30 atom percent.
- Such materials are conveniently prepared in powder, wire or foil form by rapid quenching from the melt using processing techniques that are now well-known in the art.
- the present invention provides a copper based brazing alloy composition having at least partially glassy structure.
- the composition consists essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities.
- the invention provides a homogeneous ductile brazing foil having a composition consisting essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities.
- the brazing foil of this invention is at least partially glassy and consists essentially of 9 to 11 atom percent nickel, 17 to 19 atom percent phosphorus, the balance being copper and incidental impurities.
- the homogeneous brazing foil of the invention is fabricated by a process which comprises forming a melt of the composition and quenching the melt on a rotating quench wheel at a rate of least about 10 5 ° C./sec.
- an improved process for joining two or more metal parts by brazing comprises:
- the improvement comprises employing, as the filler metal, a homogeneous, copper based foil that has the composition given above.
- the filler metal foil is easily fabricable as homogeneous, ductile ribbon, which is useful for brazing as cast.
- the copper based metal foil can be stamped into complex shapes to provide braze preforms.
- the homogeneous, ductile brazing foil of the invention can be placed inside the joint prior to the brazing operation.
- Use of the homogeneous, ductile copper based foil provided by this invention also permits brazing to be accomplished by processes such as dip brazing in molten salts, which are not readily accomplished with powder or rod-type fillers.
- Glassy metal alloys are formed by cooling a melt of the desired composition at a rate of at least about 10 5 ° C./sec.
- a variety of rapid quenching techniques well known to the glassy metal alloy art, are available for producing glassy metal powders, wires, ribbon and sheet.
- a particular composition is selected, powders or granules of the requisite elements in the desired portions are melted and homogenized, and the molten alloy is rapidly quenched on a chill surface, such as a rapidly rotating cylinder, or in a suitable fluid medium, such as water.
- Copper based brazing alloys have been fabricated by processes such as those described above. These alloys have at least partially glassy structure and consist essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities.
- Glassy Cu-Ni-P alloys of the present invention demonstrate hardness values of approximately 430 to 700 kg/mm 2 (Vickers DPH microhardness). This range is generally lower than the 600-1000 kg/mm 2 range exhibited by the transition metal-metalloid glasses described in Chen et al. or in Polk et al., U.S. Pat. No. 4,052,201, issued Oct. 4, 1977, in which iron, nickel, cobalt and/or chromium are the principal transition metals and boron, carbon, silicon, phosphorus and aluminum are the principal metalloid elements.
- the crystallization temperature of a metallic glass, Tc can be determined by differential thermal analysis (DTA).
- DTA differential thermal analysis
- the latter process involves slowly heating a glassy metal alloy and noting where excess heat is evolved over a limited temperature range.
- the glassy Cu-Ni-P alloys of this invention demonstrate initial crystallization temperatures in the range of approximately 190° to 270° C.
- the transition metal-metalloid glassy alloys described in Chen et al. and Polk et al. generally demonstrate initial crystallization temperatures of 400° to 500° C.
- the DTA process is also used to determine the melting and solidification behavior of metal alloys.
- the Cu-Ni-P compositions of the present invention have liquidus temperatures ranging from approximately 670° to 820° C. during the heating step.
- the transition metal-metalloid alloys described in Chen et al. and Polk et al. on the other hand, have liquidus temperatures ranging from approximately 900° C. to over 1200° C. during the heating step.
- the alloys taught by Chen et al. and Polk et al., as well as pure copper and the BCuP brazing alloys set forth below in Table I have liquidus temperatures substantially higher than those contained by the alloys of the present invention. As a result, the alloys of this invention are better suited for brazing than the prior art BCuP alloys or the alloys of Chen et al. or Polk et al.
- the brazing material In any brazing process, the brazing material must have a melting point that will be sufficiently high to provide strength to meet service requirements of the metal parts brazed together. However, the melting point must not be so high as to make difficult the brazing operation. Further, the filler material must be compatible, both chemically and metallurgically, with the materials being brazed. The brazing material must be more noble than the metals being brazed to avoid corrosion. Ideally, the brazing material must be in ductile foil form so that complex shapes may be stamped therefrom. Finally, the brazing foil should be homogeneous, that is, contain no binders or other materials that would otherwise form voids or contaminating residues during brazing.
- a homogeneous, ductile brazing material in foil form is provided.
- the brazing foil has a composition consisting essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus and the balance essentially copper and incidental impurities. These compositions are compatible with copper and copper-based alloys and are particularly suited for joining these materials.
- homogeneous is meant that the foil, as produced, is of substantially uniform composition in all dimensions.
- ductile is meant that foil can be bent to a round radius as small as ten times the foil thickness without fracture.
- brazing alloy compositions within the scope of the invention are set forth in Table II below.
- composition range that is compatible with and permits brazing of copper and a wide range of copper alloys under a wide range of atmospheric conditions. Such preferred composition range permits copper and copper alloys to be joined under substantially all brazing conditions.
- the preferred composition range consists essentially of 9 to 11 atom percent nickel, 17 to 19 atom percent phosphorus, the balance being essentially copper and incidental impurities.
- an improved process for joining two or more metal parts comprises:
- the improvement comprises employing, as the filler metal, at least one homogeneous, copper based foil having a composition within the ranges given above.
- the brazing foils of the invention are prepared from the melt in the same manner as glassy metal foils. Under these quenching conditions, a metastable, homogeneous, ductile material is obtained.
- the metastable material may be glassy, in which case there is no long range order.
- X-ray diffraction patterns of glassy metal alloys show only a diffuse halo, similar to that observed for inorganic oxide glasses.
- Such glassy alloys should be at least 50% glassy to be sufficiently ductile to permit subsequent handling, such as stamping complex shapes from ribbons of the alloys.
- the glassy metal alloys should be totally glassy, to attain superior ductility.
- the metastable phase may also be a solid solution of the constituent elements.
- such metastable, solid solution phases are not ordinarily produced under conventional processing techniques employed in the art of fabricating crystalline alloys.
- X-ray diffraction patterns of the solid solution alloys show the sharp diffraction peaks characteristic of crystalline alloys, with some broadening of the peaks due to desired fine-grained size of crystallites.
- Such metastable materials may also be ductile when produced under the conditions described above.
- the brazing material of the invention is advantageously produced in foil (or ribbon) form, and may be used in brazing applications as cast, whether the material is glassy or a solid solution.
- foils of glassy metal alloys may be heat treated to obtain a crystalline phase, preferably fine-grained, in order to promote longer die life when stamping of complex shapes is contemplated.
- Foils as produced by the processing described above typically are about 0.0010 to 0.0025 inch thick, which is also the desired spacing between bodies being brazed. Such spacing maximizes the strength of the braze joint. Thinner foils stacked to form greater thicknesses may also be employed. Further, no fluxes are required during brazing, and no binders are present in the foil. Thus, formation of voids and contaminating residues is eliminated. Consequently, the ductile brazing ribbons of the invention provide both ease of brazing, by eliminating the need for spacers, and minimal post-brazing treatment.
- the brazing foils of the invention are also superior to various powder brazes of the same composition in providing good braze joints. This is probably due to the ability to apply the brazing foil where the braze is required, rather than depending on capillarity to transport braze filler from the edge of surfaces to be brazed.
- Ribbons about 2.5 to 6.5 mm (about 0.10 to 0.25 inch) wide and about 25 to 60 ⁇ m about (about 0.0010 to 0.0025 inch) thick were formed by squirting a melt of the particular composition by overpressure of argon onto a rapidly rotating copper chill wheel (surface speed about 3000 to 6000 ft/min).
- Metastable, homogeneous alloy ribbons having at least partially glassy atomic structure and consisting essentially of the following compositions in atom percent were produced:
- the initial crystallization temperature (Tc) and the solidus (Ts) and liquidus (Tl) temperatures of selected ribbons from Example 1 were determined by DTA. The results of the DTA are set forth below:
- Lap shear test specimens were prepared according to AWS C 3.2 "Standard Method for Evaluating the Strength of Brazed Joints". Copper sheet, 1/8 inch thick, was used as the base metal. Glassy metal Cu 72 Ni 10 P 18 ribbon 0.0011 inch thick and 0.250 inch wide was used as the brazing filler metal. Brazed joints of the lap type were prepared. The lap dimension was carefully controlled at 3/8 inch (3 ⁇ thickness of the base metal). Brazing was done in a belt furnace with a dry, cracked ammonia atmosphere. The furnace was operated at 1350° F. (732° C.) at 1 ft/min. The length of the hot zone was 8 ft.
- BCuP-5 foil 0.0010 inch thick as a filler metal (Metbraze® 15, manufactured by Metz Metallurgical Corp., S. Plainfield, N.J.).
- Methodbraze® 15 manufactured by Metz Metallurgical Corp., S. Plainfield, N.J.
- BCuP-5 is the only BCuP alloy available in foil form suitable for the production of thin, 0.0010 to 0.0025 inch, joints.
- BCuP-5 produces joints with the greatest shear strengths (K. Weigert, The Welding Journal, V. 35, 1956, pg. 672 to 674).
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Continuous Casting (AREA)
Abstract
Novel glassy metal alloys and the brazing of metal parts employing a homogeneous ductile filler metal foil of these alloys is disclosed. The glassy metal alloys have a composition consisting essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus with the balance being copper and incidental impurities. These alloys can be produced in the form of foil useful for brazing metal articles, particularly articles composed of copper and copper alloys.
Description
1. Field of the Invention
This invention relates to copper based metal alloys and more particularly to a homogeneous, ductile brazing material useful for brazing metal articles such as those composed of copper and copper alloys.
2. Description of the Prior Art
Brazing is a process for joining metal parts, often of dissimilar composition, to each other. Typically, a filler metal that has a melting point lower than that of the metal parts to be joined together is interposed between the metal parts to form an assembly. The assembly is then heated to a temperature sufficient to melt the filler metal. Upon cooling, a strong, corrosion resistant, leaktight joint is formed.
The brazing alloys suitable for use with copper and copper alloys, designated AWS BCuP are well known compositions. These alloys contain a substantial amount (about 5 to 7.5 weight percent) of the metalloid element phosphorus. Consequently, such alloys are very brittle and are available only as powder or cast rod. Powders are generally unsuitable for many brazing operations, such as dip brazing, and do not easily permit brazing of complex shapes. Although some powders are available as pastes employing organic binders, the binders form objectionable voids and residues during brazing. Rods must be melted outside the joint and, when molten, are fed into the joint by capillary action.
Some brazing alloys are available in foil form. However, such materials are either fabricated only through a costly sequence of rolling and careful heat-treating steps or are prepared by powder metallurgical techniques. Rolled foil is not sufficiently ductile to permit stamping of complex shapes therefrom. Powder metallurgical foil is not homogeneous and employes binders, which form objectionable voids and residues during brazing.
Ductile glassy metal alloys have been disclosed in U.S. Pat. No. 3,856,513, issued Dec. 24, 1974 to H. S. Chen et al. These alloys include compositions having the formula Ti Xj, where T is at least one transition metal and X is an element selected from the group consisting of phosphorus, boron, carbon, aluminum, silicon, tin, germanium, indium, beryllium and antimony, "i" ranges from about 70 to about 87 atom percent and "j" ranges from about 13 to 30 atom percent. Such materials are conveniently prepared in powder, wire or foil form by rapid quenching from the melt using processing techniques that are now well-known in the art. However, no liquid-quenched glassy metal alloys of the family Ti Xj described above, containing copper as the principal transition metal have been reported. Chen et al. report only one copper containing composition (e.g. Pd77.5 Cu6 Si16.5) in U.S. Pat. No. 3,856,513. H. Suto and H. Ishikawa, Trans. Japan Inst. of Metals, V. 17, 1976, p. 596, report fabrication of glassy Cu-Si by vapor deposition.
There remains a need in the art for a homogeneous, copper based brazing material that is available in ductile foil form.
The present invention provides a copper based brazing alloy composition having at least partially glassy structure. The composition consists essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities.
In addition, the invention provides a homogeneous ductile brazing foil having a composition consisting essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities. Preferably, the brazing foil of this invention is at least partially glassy and consists essentially of 9 to 11 atom percent nickel, 17 to 19 atom percent phosphorus, the balance being copper and incidental impurities.
The homogeneous brazing foil of the invention is fabricated by a process which comprises forming a melt of the composition and quenching the melt on a rotating quench wheel at a rate of least about 105 ° C./sec.
Further, there is provided in accordance with the invention, an improved process for joining two or more metal parts by brazing. The process comprises:
(a) interposing a filler metal between the metal parts to form an assembly, the filler metal having a melting temperature less than that of any of the metal parts;
(b) heating the assembly to at least the melting temperature of the filler metal; and
(c) cooling the assembly.
The improvement comprises employing, as the filler metal, a homogeneous, copper based foil that has the composition given above.
The filler metal foil is easily fabricable as homogeneous, ductile ribbon, which is useful for brazing as cast. Advantageously, the copper based metal foil can be stamped into complex shapes to provide braze preforms.
Advantageously, the homogeneous, ductile brazing foil of the invention can be placed inside the joint prior to the brazing operation. Use of the homogeneous, ductile copper based foil provided by this invention also permits brazing to be accomplished by processes such as dip brazing in molten salts, which are not readily accomplished with powder or rod-type fillers.
Glassy metal alloys are formed by cooling a melt of the desired composition at a rate of at least about 105 ° C./sec. A variety of rapid quenching techniques, well known to the glassy metal alloy art, are available for producing glassy metal powders, wires, ribbon and sheet. Typically, a particular composition is selected, powders or granules of the requisite elements in the desired portions are melted and homogenized, and the molten alloy is rapidly quenched on a chill surface, such as a rapidly rotating cylinder, or in a suitable fluid medium, such as water.
Copper based brazing alloys have been fabricated by processes such as those described above. These alloys have at least partially glassy structure and consist essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities.
Glassy Cu-Ni-P alloys of the present invention demonstrate hardness values of approximately 430 to 700 kg/mm2 (Vickers DPH microhardness). This range is generally lower than the 600-1000 kg/mm2 range exhibited by the transition metal-metalloid glasses described in Chen et al. or in Polk et al., U.S. Pat. No. 4,052,201, issued Oct. 4, 1977, in which iron, nickel, cobalt and/or chromium are the principal transition metals and boron, carbon, silicon, phosphorus and aluminum are the principal metalloid elements.
The crystallization temperature of a metallic glass, Tc, can be determined by differential thermal analysis (DTA). The latter process involves slowly heating a glassy metal alloy and noting where excess heat is evolved over a limited temperature range. Upon being subjected to the DTA process, the glassy Cu-Ni-P alloys of this invention demonstrate initial crystallization temperatures in the range of approximately 190° to 270° C. By comparison, the transition metal-metalloid glassy alloys described in Chen et al. and Polk et al. generally demonstrate initial crystallization temperatures of 400° to 500° C.
The DTA process is also used to determine the melting and solidification behavior of metal alloys. When subjected to the DTA process, the Cu-Ni-P compositions of the present invention have liquidus temperatures ranging from approximately 670° to 820° C. during the heating step. The transition metal-metalloid alloys described in Chen et al. and Polk et al., on the other hand, have liquidus temperatures ranging from approximately 900° C. to over 1200° C. during the heating step. The alloys taught by Chen et al. and Polk et al., as well as pure copper and the BCuP brazing alloys set forth below in Table I have liquidus temperatures substantially higher than those contained by the alloys of the present invention. As a result, the alloys of this invention are better suited for brazing than the prior art BCuP alloys or the alloys of Chen et al. or Polk et al.
TABLE I
______________________________________
BCuP BRAZING FILLER METALS
(American Welding Society A5.8 Specifications)
Alloy Composition Brazing
Designa-
(wt. %) Solidus Liquidus
Range
tion Cu Ag P (C) (C) (C)
______________________________________
BCuP-1 Bal -- 5. 710 924 788-927
BCuP-2 " -- 7.2 710 793 732-843
BCuP-3 " 5. 6.0 643 813 718-816
BCuP-4 " 6. 7.2 643 718 691-788
BCuP-5 " 15. 5.0 643 802 704-816
BCuP-6 " 2. 7.0 643 788 732-816
BCuP-7 " 5. 6.7 643 771 704-816
______________________________________
In any brazing process, the brazing material must have a melting point that will be sufficiently high to provide strength to meet service requirements of the metal parts brazed together. However, the melting point must not be so high as to make difficult the brazing operation. Further, the filler material must be compatible, both chemically and metallurgically, with the materials being brazed. The brazing material must be more noble than the metals being brazed to avoid corrosion. Ideally, the brazing material must be in ductile foil form so that complex shapes may be stamped therefrom. Finally, the brazing foil should be homogeneous, that is, contain no binders or other materials that would otherwise form voids or contaminating residues during brazing.
In accordance with the invention, a homogeneous, ductile brazing material in foil form is provided. The brazing foil has a composition consisting essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus and the balance essentially copper and incidental impurities. These compositions are compatible with copper and copper-based alloys and are particularly suited for joining these materials.
By homogeneous is meant that the foil, as produced, is of substantially uniform composition in all dimensions. By ductile is meant that foil can be bent to a round radius as small as ten times the foil thickness without fracture.
Examples of brazing alloy compositions within the scope of the invention are set forth in Table II below.
TABLE II
______________________________________
Composition, atom %
Cu Ni P
______________________________________
1 75 10 15
2 72 10 18
3 60 20 20
4 57 30 18
______________________________________
Within the broad range disclosed above, there is a preferred composition range that is compatible with and permits brazing of copper and a wide range of copper alloys under a wide range of atmospheric conditions. Such preferred composition range permits copper and copper alloys to be joined under substantially all brazing conditions. The preferred composition range consists essentially of 9 to 11 atom percent nickel, 17 to 19 atom percent phosphorus, the balance being essentially copper and incidental impurities.
Further, in accordance with the invention, an improved process for joining two or more metal parts is disclosed. The process comprises:
(a) interposing a filler metal between the metal parts to form an assembly, the filler metal having a melting temperature less than that of any of the metal parts;
(b) heating the assembly to at least the melting temperature of the filler metal; and
(c) cooling the assembly.
The improvement comprises employing, as the filler metal, at least one homogeneous, copper based foil having a composition within the ranges given above.
The brazing foils of the invention are prepared from the melt in the same manner as glassy metal foils. Under these quenching conditions, a metastable, homogeneous, ductile material is obtained. The metastable material may be glassy, in which case there is no long range order. X-ray diffraction patterns of glassy metal alloys show only a diffuse halo, similar to that observed for inorganic oxide glasses. Such glassy alloys should be at least 50% glassy to be sufficiently ductile to permit subsequent handling, such as stamping complex shapes from ribbons of the alloys. Preferably, the glassy metal alloys should be totally glassy, to attain superior ductility.
The metastable phase may also be a solid solution of the constituent elements. In the case of the alloys of the invention, such metastable, solid solution phases are not ordinarily produced under conventional processing techniques employed in the art of fabricating crystalline alloys. X-ray diffraction patterns of the solid solution alloys show the sharp diffraction peaks characteristic of crystalline alloys, with some broadening of the peaks due to desired fine-grained size of crystallites. Such metastable materials may also be ductile when produced under the conditions described above.
The brazing material of the invention is advantageously produced in foil (or ribbon) form, and may be used in brazing applications as cast, whether the material is glassy or a solid solution. Alternatively, foils of glassy metal alloys may be heat treated to obtain a crystalline phase, preferably fine-grained, in order to promote longer die life when stamping of complex shapes is contemplated.
Foils as produced by the processing described above typically are about 0.0010 to 0.0025 inch thick, which is also the desired spacing between bodies being brazed. Such spacing maximizes the strength of the braze joint. Thinner foils stacked to form greater thicknesses may also be employed. Further, no fluxes are required during brazing, and no binders are present in the foil. Thus, formation of voids and contaminating residues is eliminated. Consequently, the ductile brazing ribbons of the invention provide both ease of brazing, by eliminating the need for spacers, and minimal post-brazing treatment.
The brazing foils of the invention are also superior to various powder brazes of the same composition in providing good braze joints. This is probably due to the ability to apply the brazing foil where the braze is required, rather than depending on capillarity to transport braze filler from the edge of surfaces to be brazed.
Ribbons about 2.5 to 6.5 mm (about 0.10 to 0.25 inch) wide and about 25 to 60 μm about (about 0.0010 to 0.0025 inch) thick were formed by squirting a melt of the particular composition by overpressure of argon onto a rapidly rotating copper chill wheel (surface speed about 3000 to 6000 ft/min). Metastable, homogeneous alloy ribbons having at least partially glassy atomic structure and consisting essentially of the following compositions in atom percent were produced:
______________________________________
Composition (atom %)
Sample No.
Cu Ni P
______________________________________
1 75 7 18
2 75 10 15
3 72 10 18
4 67 15 18
5 62 20 18
6 52 30 18
7 70 10 20
8 60 20 20
______________________________________
Selected ribbons from Example 1 were tested for Vickers diamond pyramid hardness (DPH) with the following results:
______________________________________
Composition
(Atom %) DPH
Sample No.
Cu Ni P (Kg/mm.sup.2)
______________________________________
1 75 10 15 521
2 72 10 18 435
3 67 15 18 464
4 62 20 18 473
5 57 30 18 677
6 60 20 20 526
______________________________________
The initial crystallization temperature (Tc) and the solidus (Ts) and liquidus (Tl) temperatures of selected ribbons from Example 1 were determined by DTA. The results of the DTA are set forth below:
______________________________________
Composition
(atom %) Tc* Ts** Tl**
Sample No.
Cu Ni P (°C.)
(°C.)
(°C.)
______________________________________
1 75 10 15 219 632 678
2 72 10 18 194 630 690
3 67 15 18 229 632 714
4 62 20 18 262 632 744
5 52 30 18 268 629 814
6 60 20 20 225 629 707
______________________________________
*heating rate of 20° C./sec.
**heating rate of 10° C./sec.
Lap shear test specimens were prepared according to AWS C 3.2 "Standard Method for Evaluating the Strength of Brazed Joints". Copper sheet, 1/8 inch thick, was used as the base metal. Glassy metal Cu72 Ni10 P18 ribbon 0.0011 inch thick and 0.250 inch wide was used as the brazing filler metal. Brazed joints of the lap type were prepared. The lap dimension was carefully controlled at 3/8 inch (3×thickness of the base metal). Brazing was done in a belt furnace with a dry, cracked ammonia atmosphere. The furnace was operated at 1350° F. (732° C.) at 1 ft/min. The length of the hot zone was 8 ft.
For comparison, identical joints were prepared using BCuP-5 foil 0.0010 inch thick as a filler metal (Metbraze® 15, manufactured by Metz Metallurgical Corp., S. Plainfield, N.J.). BCuP-5 is the only BCuP alloy available in foil form suitable for the production of thin, 0.0010 to 0.0025 inch, joints. Of the BCuP alloys, BCuP-5 produces joints with the greatest shear strengths (K. Weigert, The Welding Journal, V. 35, 1956, pg. 672 to 674).
Mechanical properties of the brazed joints are given below:
______________________________________
Shear Tensile
Sample Brazing Strength Strength
No. Foil (psi) (psi)
______________________________________
1 BCuP-5 8,925 26,774
2 Cu.sub.72 Ni.sub.10 P.sub.18
8,172 24,516
3 BCuP-5 7,634 22,903
4 Cu.sub.72 Ni.sub.10 P.sub.18
7,796 23,387
5 BCuP-5 8,280 24,839
6 Cu.sub.72 Ni.sub.10 P.sub.18
7,043 21,129
7 Cu.sub.72 Ni.sub.10 P.sub.18
7,796 23,387
8 BCuP-5 7,796 23,387
______________________________________
BCuP-5 Cu.sub.72 Ni.sub.10 P.sub.18
______________________________________
Ave. Shear Strength
8,159 psi 7,702 psi
sigma = 580 sigma = 474
Ave. Tensile Strength
24,476 psi 23,105 psi
sigma = 1739 sigma = 1421
______________________________________
Analyses of the mechanical properties data indicate that no differences of statistical significance exist between joints bonded with BCuP-5 foil and joints bonded with Cu72 Ni10 P18 foil.
Having thus described the invention in rather full detail, it will be understood that these details need not be strictly adhered to but that further modifications of the invention may suggest themselves to one skilled in the art, all falling within the scope of the invention as defined by the subjoined claims.
Claims (5)
1. A homogeneous ductile brazing foil having at least partially glassy structure and a composition consisting essentially of 5 to 40 atom percent nickel, 15 to 20 atom percent phosphorus, the balance being copper and incidental impurities.
2. A homogeneous brazing foil having a composition consisting essentially of 9 to 11 atom percent nickel, 17 to 19 atom percent phosphorus, the balance being copper and incidental impurities.
3. A brazing foil as recited in claim 1, said foil having a thickness ranging from about 0.0010 to 0.0025 inch.
4. A brazing foil as recited in claim 1, said foil having at least about 50% glassy structure.
5. A brazing foil as recited in claim 1, said foil having totally glassy structure.
Priority Applications (9)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/947,329 US4209570A (en) | 1978-10-02 | 1978-10-02 | Homogeneous brazing foils of copper based metallic glasses |
| AU50463/79A AU524998B2 (en) | 1978-10-02 | 1979-08-31 | Homogeneous brazing foils of cu. based metallic glasses |
| CA336,249A CA1123632A (en) | 1978-10-02 | 1979-09-24 | Homogeneous brazing foils of copper based metallic glasses |
| EP79302046A EP0010866B1 (en) | 1978-10-02 | 1979-09-28 | Homogeneous brazing foils of copper based metallic glasses |
| DE7979302046T DE2965450D1 (en) | 1978-10-02 | 1979-09-28 | Homogeneous brazing foils of copper based metallic glasses |
| JP54127253A JPS599274B2 (en) | 1978-10-02 | 1979-10-02 | Homogeneous brazing foil of copper-based amorphous metal |
| US06/088,431 US4253870A (en) | 1978-10-02 | 1979-10-26 | Homogeneous brazing foils of copper based metallic glasses |
| US06/170,249 US4316573A (en) | 1978-10-02 | 1980-07-18 | Homogeneous brazing foils of copper based metallic glasses |
| JP58070843A JPS5929661B2 (en) | 1978-10-02 | 1983-04-21 | Copper-based amorphous homogeneous alloy |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/947,329 US4209570A (en) | 1978-10-02 | 1978-10-02 | Homogeneous brazing foils of copper based metallic glasses |
| US06/088,431 US4253870A (en) | 1978-10-02 | 1979-10-26 | Homogeneous brazing foils of copper based metallic glasses |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/088,431 Division US4253870A (en) | 1978-10-02 | 1979-10-26 | Homogeneous brazing foils of copper based metallic glasses |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US4209570A true US4209570A (en) | 1980-06-24 |
Family
ID=26778651
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US05/947,329 Expired - Lifetime US4209570A (en) | 1978-10-02 | 1978-10-02 | Homogeneous brazing foils of copper based metallic glasses |
| US06/088,431 Expired - Lifetime US4253870A (en) | 1978-10-02 | 1979-10-26 | Homogeneous brazing foils of copper based metallic glasses |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/088,431 Expired - Lifetime US4253870A (en) | 1978-10-02 | 1979-10-26 | Homogeneous brazing foils of copper based metallic glasses |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US4209570A (en) |
| EP (1) | EP0010866B1 (en) |
| JP (2) | JPS599274B2 (en) |
| AU (1) | AU524998B2 (en) |
| CA (1) | CA1123632A (en) |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4448853A (en) * | 1981-04-15 | 1984-05-15 | Bbc Brown, Boveri & Company, Limited | Layered active brazing material and method for producing it |
| US4448851A (en) * | 1982-09-20 | 1984-05-15 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4448852A (en) * | 1982-09-20 | 1984-05-15 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4460658A (en) * | 1982-09-20 | 1984-07-17 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4489136A (en) * | 1982-09-20 | 1984-12-18 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4497429A (en) * | 1982-09-20 | 1985-02-05 | Allied Corporation | Process for joining together two or more metal parts using a homogeneous low melting point copper based alloys |
| US4522331A (en) * | 1983-06-03 | 1985-06-11 | Allied Corporation | Method of brazing with low melting point copper-tin foils |
| US4562951A (en) * | 1982-04-12 | 1986-01-07 | The United States Of America As Represented By The Secretary Of The Army | Method of making metallic glass-metal matrix composites |
| US4573630A (en) * | 1983-04-26 | 1986-03-04 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4621031A (en) * | 1984-11-16 | 1986-11-04 | Dresser Industries, Inc. | Composite material bonded by an amorphous metal, and preparation thereof |
| US4626296A (en) * | 1985-02-11 | 1986-12-02 | The United States Of America As Represented By The United States Department Of Energy | Synthesis of new amorphous metallic spin glasses |
| US4654275A (en) * | 1985-11-27 | 1987-03-31 | Allied Corporation | Storage life of Pb-In-Ag solder foil by Sn addition |
| US4756747A (en) * | 1985-02-11 | 1988-07-12 | The United States Of America As Represented By The Department Of Energy | Synthesis of new amorphous metallic spin glasses |
| US4929511A (en) * | 1983-12-06 | 1990-05-29 | Allied-Signal Inc. | Low temperature aluminum based brazing alloys |
| US5064611A (en) * | 1990-04-26 | 1991-11-12 | Mitsubishi Denki Kabushiki Kaisha | Process for producing copper alloy |
| US5378294A (en) * | 1989-11-17 | 1995-01-03 | Outokumpu Oy | Copper alloys to be used as brazing filler metals |
| US20050072830A1 (en) * | 2003-10-04 | 2005-04-07 | Siemens Westinghouse Power Corporation | Consumable insert and method of using the same |
| CN100408713C (en) * | 2006-11-04 | 2008-08-06 | 燕山大学 | Bulk binary NiP amorphous alloy and preparation method thereof |
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| EP0038584B1 (en) * | 1980-04-21 | 1984-08-15 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Multi-layered-solder and method of producing such solder |
| DE3106607C2 (en) * | 1981-02-23 | 1987-08-20 | Fr. Kammerer GmbH, 7530 Pforzheim | Plating process |
| JPS58148094A (en) * | 1982-02-25 | 1983-09-03 | Tanaka Kikinzoku Kogyo Kk | Brazing filler metal |
| US5084251A (en) * | 1989-10-26 | 1992-01-28 | Thomas Akatheputhethu C | Instrument sterilization cassette |
| FI87470C (en) * | 1989-11-17 | 1993-01-11 | Outokumpu Oy | SOM SLAGLOD ANVAENDBARA KOPPARLEGERINGAR |
| JP4077888B2 (en) * | 1995-07-21 | 2008-04-23 | 株式会社東芝 | Ceramic circuit board |
| DE10335947A1 (en) | 2003-08-04 | 2005-03-17 | Vacuumschmelze Gmbh & Co. Kg | Copper brazing alloy and brazing method |
| DE102006058376A1 (en) * | 2006-12-08 | 2008-04-30 | Vacuumschmelze Gmbh & Co. Kg | Brazing foil comprises metal foil containing solder and with layer of adhesive on one or both sides |
| JP2019157202A (en) | 2018-03-13 | 2019-09-19 | 三菱重工業株式会社 | Repair method of ceramic coating, ceramic coating, turbine member and gas turbine |
| DE102019122524A1 (en) * | 2019-08-21 | 2021-02-25 | Vacuumschmelze Gmbh & Co. Kg | Amorphous metal foil and method for producing an amorphous metal foil with a rapid solidification technology |
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| US2606362A (en) * | 1947-10-29 | 1952-08-12 | United Aircraft Corp | Method of maintaining the desired joint thickness during a soldering operation |
| US3871836A (en) * | 1972-12-20 | 1975-03-18 | Allied Chem | Cutting blades made of or coated with an amorphous metal |
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| US2911298A (en) * | 1958-02-11 | 1959-11-03 | Air Preheater | Copper base brazing alloy |
| DE1533192A1 (en) * | 1966-11-30 | 1970-04-23 | Winter Dr Heinrich | Process for the production of alloys for soldering, contacting and / or doping semiconductors |
| DE2241342B2 (en) * | 1972-08-23 | 1974-06-20 | Metallgesellschaft Ag, 6000 Frankfurt | Method for soldering metals, in particular copper and / or alloys containing copper |
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Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4448853A (en) * | 1981-04-15 | 1984-05-15 | Bbc Brown, Boveri & Company, Limited | Layered active brazing material and method for producing it |
| US4562951A (en) * | 1982-04-12 | 1986-01-07 | The United States Of America As Represented By The Secretary Of The Army | Method of making metallic glass-metal matrix composites |
| US4448851A (en) * | 1982-09-20 | 1984-05-15 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4448852A (en) * | 1982-09-20 | 1984-05-15 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4460658A (en) * | 1982-09-20 | 1984-07-17 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4489136A (en) * | 1982-09-20 | 1984-12-18 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4497429A (en) * | 1982-09-20 | 1985-02-05 | Allied Corporation | Process for joining together two or more metal parts using a homogeneous low melting point copper based alloys |
| US4573630A (en) * | 1983-04-26 | 1986-03-04 | Allied Corporation | Homogeneous low melting point copper based alloys |
| US4522331A (en) * | 1983-06-03 | 1985-06-11 | Allied Corporation | Method of brazing with low melting point copper-tin foils |
| US4929511A (en) * | 1983-12-06 | 1990-05-29 | Allied-Signal Inc. | Low temperature aluminum based brazing alloys |
| US4621031A (en) * | 1984-11-16 | 1986-11-04 | Dresser Industries, Inc. | Composite material bonded by an amorphous metal, and preparation thereof |
| US4626296A (en) * | 1985-02-11 | 1986-12-02 | The United States Of America As Represented By The United States Department Of Energy | Synthesis of new amorphous metallic spin glasses |
| US4756747A (en) * | 1985-02-11 | 1988-07-12 | The United States Of America As Represented By The Department Of Energy | Synthesis of new amorphous metallic spin glasses |
| US4654275A (en) * | 1985-11-27 | 1987-03-31 | Allied Corporation | Storage life of Pb-In-Ag solder foil by Sn addition |
| US5378294A (en) * | 1989-11-17 | 1995-01-03 | Outokumpu Oy | Copper alloys to be used as brazing filler metals |
| US5064611A (en) * | 1990-04-26 | 1991-11-12 | Mitsubishi Denki Kabushiki Kaisha | Process for producing copper alloy |
| US20050072830A1 (en) * | 2003-10-04 | 2005-04-07 | Siemens Westinghouse Power Corporation | Consumable insert and method of using the same |
| US7775414B2 (en) | 2003-10-04 | 2010-08-17 | Siemens Energy, Inc. | Consumable insert and method of using the same |
| CN100408713C (en) * | 2006-11-04 | 2008-08-06 | 燕山大学 | Bulk binary NiP amorphous alloy and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0010866B1 (en) | 1983-05-18 |
| JPS5550996A (en) | 1980-04-14 |
| JPS58193334A (en) | 1983-11-11 |
| US4253870A (en) | 1981-03-03 |
| JPS5929661B2 (en) | 1984-07-21 |
| CA1123632A (en) | 1982-05-18 |
| JPS599274B2 (en) | 1984-03-01 |
| AU524998B2 (en) | 1982-10-14 |
| AU5046379A (en) | 1980-04-17 |
| EP0010866A1 (en) | 1980-05-14 |
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